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For|the band|M.I.R.V.A multiple independently targetable reentry vehicle ( MIRV ) warhead is a collection of nuclear weapon s carried on a single intercontinental ballistic missile (ICBM) or a submarine-launched ballistic missile (SLBM). Using a MIRV warhead, a single launched missile can strike several targets individually, or fewer targets redundantly. By contrast a unitary warhead is a single warhead on a single missile.
Purpose
The military purpose of a MIRV is threefold:
Provides greater target damage for a given missile payload. Radiation (including radiated heat) from a nuclear warhead diminishes as the square of the distance (called the inverse-square law ), and blast pressure diminishes as the cube of the distance. For example at a distance of 4& nbsp;km from ground zero, the blast pressure is only 1/64th that of 1& nbsp;km. Due to these effects several small warheads cause much more target damage area than a single large one. This in turn reduces the number of missiles and launch facilities required for a given destruction level - much the same as the purpose of a conventional explosive|conventional submunition .
With single warhead missiles, one missile must be launched for each target. By contrast with a MIRV warhead, the post-boost (or bus) stage can dispense the warheads against multiple targets across a broad area.
Reduces the effectiveness of an anti-ballistic missile system that relies on intercepting individual warheads. While a MIRV attacking missile can have multiple (3–12 on United States missiles and 3-10 on Russians) warheads, interceptors may have only one warhead per missile. Thus, in both a military and an economic sense, MIRVs render ABM systems less effective, as the costs of maintaining a workable defense against MIRVs would greatly increase, requiring multiple defensive missiles for each offensive one. Decoy reentry vehicles can be used alongside actual warheads to minimize the chances of the actual warheads being intercepted before they reach their targets. A system that destroys the missile earlier in its trajectory (before MIRV separation) is not affected by this but is more difficult, and thus more expensive to implement.
Cause more the maximum amount of damage using the least amount of missiles.
MIRV land-based ICBMs were considered destabilizing because they tended to put a premium on first-strike|striking first . The world's first MIRV—US Minuteman III missile of 1970—threatened to rapidly increase the US's deployable nuclear arsenal and thus the possibility that it would have enough bombs to destroy virtually all of the Soviet Union 's nuclear weapons and negate any significant retaliation. Later on the US feared the Soviet's MIRVs because Soviet missiles had a greater throw-weight and could thus put more warheads on each missile than the US could. For example the US MIRVs might have increased their warhead per missile count by a factor of 6 while the Soviets increased theirs by a factor of 10. Furthermore, the US had a much smaller proportion of its nuclear arsenal in ICBMs than the Soviets. Bombers could not be outfitted with MIRVs so their capacity would not be multiplied. Thus the US did not seem to have as much potential for MIRV usage as the Soviets. However, the US had a larger number of SLBM s, which could be outfitted with MIRVs, and helped offset the ICBM disadvantage. It is because of this that this type of weapon was banned under the START II agreement. However, START II was never ratified by the Russian Duma due to disagreements about the Anti-Ballistic Missile Treaty|ABM Treaty .
The Russia|Russian Federation claims to have developed the most advanced MIRV system as of 2006 for use in the RSM-56 Bulava .Citation needed|date=November 2009
Mode of operation
In a MIRV, the main rocket motor (or Rocket booster|booster ) pushes a "bus" (see illustration) into a free-flight suborbital ballistic flight path. After the boost phase the bus maneuvers using small on-board rocket motors and a computerised inertial guidance system . It takes up a ballistic trajectory that will deliver a Atmospheric reentry|reentry vehicle containing a Nuclear warhead|warhead to a target, and then releases a warhead on that trajectory. It then maneuvers to a different trajectory, releasing another warhead, and repeats the process for all warheads.
1. The missile launches out of its silo by firing its first stage boost motor ( A ). 2. About 60 seconds after launch, the 1st stage drops off and the second stage motor ( B ) ignites. The missile shroud ( E ) is ejected. 3. About 120 seconds after launch, the third stage motor ( C ) ignites and separates from the 2nd stage. 4. About 180 seconds after launch, third stage thrust terminates and the Post-Boost Vehicle ( D ) separates from the rocket. 5. The Post-Boost Vehicle maneuvers itself and prepares for re-entry vehicle (RV) deployment. 6. While the Post-Boost Vehicle backs away, the RVs, decoys, and chaff are deployed (although the figure shows this happening during descent, this may occur during ascent instead). 7. The RVs and chaff re-enter the atmosphere at high speeds and are armed in flight. 8. The nuclear warheads detonate, either as air bursts or ground bursts.
The precise technical details are closely guarded military secret s, to hinder any development of enemy counter-measures. The bus' on-board propellant limits the distances between targets of individual warheads to perhaps a few hundred km. http://www.airliners.net/discussions/military/read.main/68181/ Question Re Mirv Warheads — Military Forum | Airliners.net Some warheads may use small hypersonic airfoils during the descent to gain additional cross-range distance. Additionally, some buses (e.g. the UK|British Chevaline system) can release decoy s to confuse interception devices and radar s, such as aluminium|aluminized balloons or electronic noisemakers.
Accuracy is crucial, because doubling the accuracy decreases the needed warhead energy by a factor of four for radiation damage and by a factor of eight for blast damage. Navigation system accuracy and the available geophysical information limits the warhead target accuracy. Some writers believe that government-supported geophysical mapping initiatives and ocean satellite altitude systems such as Seasat may have a covert purpose to map mass concentrations and determine local Gravity anomaly|gravity anomalies , in order to improve accuracies of ballistic missiles. Accuracy is expressed as circular error probable (CEP). This is simply the radius of the circle that the warhead has a 50 percent chance of falling into when aimed at the center. CEP is about 90–100 m for the Trident missile|Trident II and LGM-118A Peacekeeper|Peacekeeper missilesCitation needed|date=October 2009.
See also
Atmospheric reentry
M45 SLBM
M51 SLBM
Maneuverable reentry vehicle (MARV)
Multiple Reentry vehicle
Nuclear warfare
Poseidon missile
START II
commons|MIRV
References
reflist|2
External links
http://www.gwu.edu/~nsarchiv/nsa/NC/mirv/mirv.html "MIRV: A BRIEF HISTORY OF MINUTEMAN and MULTIPLE REENTRY VEHICLES" by Daniel Buchonnet, Lawrence Livermore Laboratory, February 1976.
